SA7024 (sa7024-il)
SA7024 - Selig / Ashok Gopalarathnam SA7024 low Reynolds number airfoil
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(sa7024-il) SA7024 Selig / Ashok Gopalarathnam SA7024 low Reynolds number airfoil Max thickness 7% at 25.9% chord. Max camber 3.3% at 43.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
SA7024
1.00000 .00000
.99820 .00029
.99296 .00127
.98456 .00298
.97328 .00531
.95928 .00803
.94257 .01096
.92315 .01411
.90116 .01753
.87679 .02117
.85023 .02497
.82165 .02889
.79126 .03288
.75924 .03686
.72579 .04078
.69115 .04460
.65551 .04824
.61909 .05166
.58210 .05481
.54479 .05763
.50733 .06007
.46996 .06212
.43289 .06369
.39632 .06477
.36045 .06535
.32549 .06539
.29159 .06485
.25893 .06376
.22772 .06210
.19806 .05986
.17009 .05707
.14398 .05377
.11982 .04993
.09767 .04563
.07768 .04094
.05989 .03587
.04433 .03049
.03104 .02498
.02012 .01940
.01158 .01386
.00540 .00851
.00158 .00354
0.0 0.0
.00166 -.00362
.00686 -.00589
.01518 -.00796
.02645 -.00964
.04065 -.01082
.05781 -.01156
.07781 -.01189
.10057 -.01180
.12597 -.01135
.15388 -.01057
.18414 -.00950
.21657 -.00818
.25098 -.00667
.28717 -.00501
.32492 -.00326
.36398 -.00147
.40410 .00029
.44502 .00196
.48645 .00350
.52813 .00484
.56970 .00589
.61079 .00666
.65110 .00720
.69038 .00752
.72834 .00763
.76472 .00754
.79926 .00727
.83172 .00682
.86187 .00624
.88949 .00555
.91441 .00479
.93644 .00397
.95544 .00313
.97125 .00228
.98372 .00146
.99273 .00074
.99818 .00021
1.00000 0.00000
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Polars for SA7024 (sa7024-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sa7024-il | 50,000 | 9 | 38.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7024-il | 50,000 | 5 | 42.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7024-il | 100,000 | 9 | 59.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7024-il | 100,000 | 5 | 59 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7024-il | 200,000 | 9 | 80.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7024-il | 200,000 | 5 | 74.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7024-il | 500,000 | 9 | 105.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7024-il | 500,000 | 5 | 93.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7024-il | 1,000,000 | 9 | 122.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7024-il | 1,000,000 | 5 | 107.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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